UA98686C2 - Deformable rear disc for missile container, including a downstream bearing frame - Google Patents

Deformable rear disc for missile container, including a downstream bearing frame

Info

Publication number
UA98686C2
UA98686C2 UAA201008714A UAA201008714A UA98686C2 UA 98686 C2 UA98686 C2 UA 98686C2 UA A201008714 A UAA201008714 A UA A201008714A UA A201008714 A UAA201008714 A UA A201008714A UA 98686 C2 UA98686 C2 UA 98686C2
Authority
UA
Ukraine
Prior art keywords
bearing frame
downstream
downstream bearing
rear disc
disc
Prior art date
Application number
UAA201008714A
Other languages
Russian (ru)
Ukrainian (uk)
Inventor
Пьер Жак Трюиман
Original Assignee
ДеСееНеС
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by ДеСееНеС filed Critical ДеСееНеС
Publication of UA98686C2 publication Critical patent/UA98686C2/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00—Rocket or torpedo launchers
    • F41F3/04—Rocket or torpedo launchers for rockets
    • F41F3/042—Rocket or torpedo launchers for rockets the launching apparatus being used also as a transport container for the rocket
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00—Rocket or torpedo launchers
    • F41F3/04—Rocket or torpedo launchers for rockets
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00—Rocket or torpedo launchers
    • F41F3/04—Rocket or torpedo launchers for rockets
    • F41F3/0413—Means for exhaust gas disposal, e.g. exhaust deflectors, gas evacuation systems

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Carbon And Carbon Compounds (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Support Of The Bearing (AREA)
  • Closures For Containers (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)

Abstract

The invention relates to an improved deformable downstream disc (56; 156; 256) to be fitted on the bottom of a container (15) for a missile (16) and including a stack of elastic blades (63) clamped between at least an upstream and a downstream thermal protection membrane and sealing membrane (70, 71, 72, 73), and maintained between an upstream bearing frame (61) and a downstream bearing frame (64), characterized in that the downstream bearing frame includes an inner edge (80) having an extension so as to provide the disc with an abutment means defining a position of maximum deformation of the elastic blades.
UAA201008714A 2008-01-11 2009-01-08 Deformable rear disc for missile container, including a downstream bearing frame UA98686C2 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0850162A FR2926360B1 (en) 2008-01-11 2008-01-11 DEFORMABLE REAR OPERATOR FOR MISSILE CONTAINER, COMPRISING A FRONT SUPPORT FRAME

Publications (1)

Publication Number Publication Date
UA98686C2 true UA98686C2 (en) 2012-06-11

Family

ID=39745427

Family Applications (1)

Application Number Title Priority Date Filing Date
UAA201008714A UA98686C2 (en) 2008-01-11 2009-01-08 Deformable rear disc for missile container, including a downstream bearing frame

Country Status (11)

Country Link
US (1) US8418593B2 (en)
EP (1) EP2229573B1 (en)
KR (1) KR101567998B1 (en)
CN (1) CN101918786B (en)
ES (1) ES2617208T3 (en)
FR (1) FR2926360B1 (en)
MA (1) MA32051B1 (en)
PL (1) PL2229573T3 (en)
UA (1) UA98686C2 (en)
WO (1) WO2009092938A2 (en)
ZA (1) ZA201004820B (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8300757B2 (en) 2008-08-08 2012-10-30 Motorola Mobility Llc Methods for detection of failure and recovery in a radio link
US8584569B1 (en) * 2011-12-06 2013-11-19 The United States Of America As Represented By The Secretary Of The Navy Plume exhaust management for VLS
FR3039889B1 (en) 2015-08-05 2017-07-28 Mbda France FLEXIBLE OPENER FOR MISSILE CONTAINER
BE1023108B1 (en) 2015-08-24 2016-11-23 Handi-Move N.V. Improved clamp and aids for lifting patients using the clamp
FR3053455B1 (en) * 2016-07-01 2019-04-19 Mbda France FLEXIBLE OPENER FOR MISSILE CONTAINER
CN112985174B (en) * 2021-02-10 2023-01-10 上海材料研究所 Cylindrical orthogonal type sealing rear end cover with rectification effect on shock wave reflection

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4324167A (en) * 1980-04-14 1982-04-13 General Dynamics, Pomona Division Flexible area launch tube rear cover
US4498368A (en) * 1983-10-06 1985-02-12 The United States Of America As Representedby The Secretary Of The Navy Frangible fly through diaphragm for missile launch canister
US4683798A (en) * 1985-12-27 1987-08-04 General Dynamics, Pomona Division Gas management transition device
US4686884A (en) * 1985-12-27 1987-08-18 General Dynamics, Pomona Division Gas management deflector
FR2620808B1 (en) 1987-09-17 1990-01-12 France Etat Armement REAR LID FOR MISSILE CONTAINER
US5194688A (en) * 1992-01-31 1993-03-16 Hughes Missile Systems Company Apparatus for limiting recirculation of rocket exhaust gases during missile launch
JP2001124494A (en) * 1999-10-25 2001-05-11 Mitsubishi Electric Corp Discharger for flier
JP4338004B2 (en) * 2000-03-16 2009-09-30 株式会社Ｉｈｉエアロスペース Rocket motor nozzle cover
JP3448648B2 (en) * 2000-11-27 2003-09-22 防衛庁技術研究本部長 Flying object launcher device
JP2004077038A (en) * 2002-08-20 2004-03-11 Mitsubishi Heavy Ind Ltd Back lid of canister for missile
US7984675B2 (en) * 2006-02-21 2011-07-26 Metal Storm Limited Propellant sealing system for stackable projectiles

Also Published As

Publication number Publication date
FR2926360A1 (en) 2009-07-17
US8418593B2 (en) 2013-04-16
US20110011251A1 (en) 2011-01-20
ES2617208T3 (en) 2017-06-15
EP2229573B1 (en) 2016-12-07
FR2926360B1 (en) 2012-10-19
KR101567998B1 (en) 2015-11-10
ZA201004820B (en) 2011-03-30
WO2009092938A3 (en) 2009-12-17
WO2009092938A2 (en) 2009-07-30
EP2229573A2 (en) 2010-09-22
MA32051B1 (en) 2011-02-01
CN101918786A (en) 2010-12-15
KR20100122899A (en) 2010-11-23
PL2229573T3 (en) 2017-05-31
CN101918786B (en) 2013-04-24

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